JASC 5753
Service difficulty reports · 31,513
Reports filed under 5753 · Trailing Edge Flaps, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5753' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5753' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IXXA20150724094Support Fitting · crackedNUMBER 8 FLAP SUPPORT FITTING HOLES NUMBERED FROM INBD TO OTBD 1 - 4. NUMBER 4 HOLE HAS A CRACK INDICATION. REAMED HOLE NR 4 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & 8755" IAW REA 47158REA03 & SRM 51-40-05SDR IXXA20150724093Support Fitting · crackedNUMBER 8 FLAP SUPPORT FITTING HOLES NUMBERED FROM INBD TO OTBD 1 - 4. NR 3 HOLE HAS A CRACK INDICATION. REAMED HOLE NR 3 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & 8755" IAW REA 47158REA03 & SRM 51-40-05.SDR IXXA20150724092Support Fitting · crackedNUMBER 8 FLAP SUPPORT FITTING HOLES NUMBERED FROM INBD TO OTBD 1 - 4. NR 2 HOLE HAS A CRACK INDICATION. REAMED HOLE NR 2 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .7495" IAW REA 47158REA03 & SRM 51-40-05.SDR IXXA20150724091Support Fitting · crackedNUMBER 8 FLAP SUPPORT FITTING NUMBERED FROM INBD TO OTBD 1 - 4. NR 1 FLAP SUPPORT BOLT SHOWS CRACK INDICATION. REAMED HOLE NR 1 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .7495" IAW REA 47158REA03 & SRM 51-40-05.SDR IXXA20150724090Support Fitting · crackedDURING INSPECTION, NR 2HOLE IS PITTED & SHOWS CRACK INDICATION. NR 2 FLAP SUPPORT FITTING NUMBERED FROM LT TO RT. REAMED HOLE NR 2 IN THE NR 2 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & .8755" IAW REA 47158REA03 & SRM 5SDR IXXA20150724089Support Fitting · corrodedDURING HFEC INSPECTION, NR 4 HOLE IS PITTED & SHOWS CRACK INDICATION. NR 2 FLAP SUPPORT FITTING NUMBERED FROM LT TO RT. REAMED HOLE NR 4 IN THE NR 2 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & .8755" IAW REA 47158REA03 &SDR IXXA20150724088Support Fitting · crackedDURING INSPECTION, NR 2 FLAP SUPPORT FITTING, NR 1 HOLE IS PITTED & SHOWS CRACK INDICATION. NR 2 FLAP SUPPORT FITTING NUMBERED FROM LT TO RT. REAMED HOLE NR 1 IN THE NR 2 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8750" IAW REASDR IXXA20150724087Support Fitting · crackedNUMBER 1 FLAP FITTING, NR 3 HOLE SHOWS CRACK INDICATION DURING HFEC INSPECTION. NR 1 FLAP SUPPORT FITTING, NUMBERING IS FROM LT TO RT. REAMED HOLE NR 3 IN THE NR 1 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .07495" & .07505" IAWSDR FDEA201506151817Repair · delaminatedAGEING INSPECTION, EXISTING REPAIR ON RT OUTER FLAP, UPPER SKIN OUT OF RIB 10 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH APPROVED DATA. BUT INSPECTION FOUND DELAMINATION ON OLD REPAIR. REPAIRED THE DAMAGSDR FDEA201506151816Repair · delaminatedAGEING INSPECTION, EXISTING REPAIR ON RT OUTER FLAP, UPPER SKIN OUT OF RIB 10 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH APPROVED DATA. BUT INSPECTION FOUND DELAMINATION ON OLD REPAIR. REPAIRED THE DAMAGSDR FDEA201506151815Skin · delaminatedAGEING INSPECTION, EXISTING REPAIR ON RT OUTER FLAP UPPER SKIN OUT OF RIB 10 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH APPROVED DATA. BUT INSPECTION FOUND DELAMINATION ON OLD REPAIR. REPAIRED THE DAMAGESDR UIEA2015061600315Fitting · damagedLEFT WING FLAP SUPPORT RIB INBD FITTING, OTBD HOLE HAS DAMAGE, NICK IN HOLE. REAMED OTBD HOLE TO .875. CONFIRMED DAMAGE REMOVAL BY NDT REAMED INBD HOLE TO .875 IAW MSG PMO-TLS-15-0013-02B OF SR 4-2892244521.SDR IPXA2015061490141Skin · damagedRIGHT INBD T/E FLAP LOWER SKIN DAMAGED. REPAIRED IAW EO B767-5750-57785-A.SDR REXA2015061300596Panel · chafedTASK CARD 900-27-580-100 INBD FLAP MOVEABLE VANE PANEL 584ET HAS CHAFE ON TOP. PANEL 584ET IS OUT OF LIMITS. R & R PANEL 584ET IAW SRM 57-52-01 & 51-40-11.SDR SWIA201541359Vane · chafedCENTER CAP OF LT INBD FLAP VANE CHAFED. R & R THE LT INBD FLAP MOVEABLE VANE CENTER CAP IAW SRM AND STS EA.SDR SWAA2015070141295Support Angle · crackedRIGHT WING FLAP TRACK INBD TE SUPPORT ANGLE INBD CRACKED. R & R ANGLE IAW SRM.SDR SWAA2015062240999Skin · delaminatedLEFT WING INBD FORE FLAP OUTER SURFACE SKIN DELAMINATED. REPAIRED SKIN IAW SRM.SDR KO0R201506120075Skin · corrodedRIGHT WING OTBD FLAP UPPER SKIN PANEL IS CORRODED.SDR KO0R201506120074Skin · crackedLEFT WING OTBD FLAP CTR BOX UPPER SKIN PANEL IS CRACKED.SDR KO0R201506120073Spar · corrodedRIGHT WING INBD MAIN FLAP AFT SPAR UPPER CHORD IS CORRODED.SDR ASAA2015061112165Skin · chafedRT WING OTBD FOREFLAP INBD L/E IS CHAFED ON PREVIOUS REPAIR. ACFT GROUNDED. REMOVED RT OTBD FOREFLAP INBD L/E SKIN AND INSTALLED NEW SKIN IAW SRM 51-40-04-0G-0-4 AND FIG 1.SDR IPXA2015062490509Skin · dentedINSPECTION TYPE:C9, LEFT INBD FLAP UPPER SURFACE IS DENTED, CREASED. REPAIRED WITH METAL HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1 AND 51-70-10, REPAIR 2.SDR IPXA2015062490505Skin · dentedINSPECTION TYPE: C9, LEFT INBD FLAP UPPER SURFACE IS DENTED, CREASED. REPAIRED WITH HOT METAL BOND REPAIR IAW SRM 57-53-01, REPAIR 1 AND 51-70-10, REPAIR 2.SDR WX0A2015061572656Vane · corrodedRIGHT WING OTBD MID FLAP HAS HOLE FROM CORROSION. R & R RT WING OTBD FLAP, OTBD FIXED VANE IAW AMM UP TO 27-51-03-2-0 STEP 3 B 3. SEE LOG PAGE 608374 FOR FINAL INSTALL & ADJUSTMENT.SDR CALA2015061193889Bar · damagedNUMBER 5 FLAP TRACK FAIL SAFE BAR DAMAGED. BUSHING & TOOLING HOLE ELONGATED. REPAIR ACP IAW 747EN-57-0184. DVI AFFECTED AREA OF FAILSAFE BAR & REPAIR BUSHING FOR CORROSION, CRACKS & OTHER REPAIR DEGRADATION AT EVERY C-CHECK, NOT TO EXCEED 24 MONTHS. SEE UASDR CALA2015061100501Flap · damagedRIGHT INBD FLAP HAS 2 EACH ELONGATED FASTENER HOLES, LOCATED INSIDE PANEL 655AR. REPAIRED 2 EACH RT INBD FLAP FASTENER HOLES IAW ECRA 5750-0 4789 SEE WIPS FOR WORK ACCOMPLISHED.SDR DALA2015061003732Vane · damagedSEVERAL NICKS ON PREVIOUS REPAIR DOUBLER AT NR 1 FLAP VANE. THE PREVIOUS DOUBLER WAS REPLACED IAW SRM 57-03D, PAR 11.SDR DALA2015060903806Angle · corrodedCORROSION ON ANGLES LOCATED ON RT WING OTBD FLAP INNER STRUCTURE, XRS 164. FLAP AND VANES WERE R & R .SDR FDEA201506081722Skin · wornLEFT INBD MAIN FLAP, OTBD NOSE SKIN WORN 36" FROM OTBD EDGE TO MOST OTBD EDGE. REPAIRED IAW EA F-5750-T0316370 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR AALA201506179010Bolt · corroded3S CHECK, CORROSION ON RT WING TE FLAP NR 3 TRACK PIVOT BOLT. REPLACED RT WING TE FLAP NR 3 TRACK PIVOT BOLT IAW 26T63257002.SDR DALA2015060903650Rib · damagedCORROSION AND SCRATCHS ON RIB HOLES NR 2 BS XOS= 240 WERE REMOVED IAW SRM 57-02 PAR 9. REWORKED HOLES WERE MEASURED INBD LUG FWD HOLE 0.939" AND AFT HOLE 0.941". BUSHINGS WERE FABRICATED IAW SRM 57-02, PAR 9, C, TABLE 1, 1, 2. BUSHINGS WITH OD 0.942" BUSHINSDR SIMA20150604003Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE HAS A DENT, ONE FOOT FROM INBD EDGE. COMPLIED WITH ERS-CR-57MR-449.SDR ASOA20150604130Fitting · crackedDURING C-CHECK, THE RT OTBD FLAP INBD TORQUE BOX FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FITTING IAW EC5750-01696. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR E4EB2015FA0000573Skin · corrodedLEFT WING INBD FLAP UPPER SURFACE INBD RUB PLATE HAS POPPED AND CRACKED RIVETS. FOUND EXFOLIATED SKIN UNDER PLATE.SDR SWAA2015062241022Skin · delaminatedLEFT WING INBD FORE FLAP DELAMINATED ON UPPER SKIN AT 49.50 FROM OTBD EDGE. REPAIRED FORE FLAP IAW SRM.SDR SWAA2015061840884Skin · delaminatedLEFT WING INBD FORE FLAP DELAMINATED ON UPPER SKIN. REPAIRED FORE FLAP IAW SRM.SDR SWAA2015061640777Skin · delaminatedLEFT WING INBD FORE FLAP DELAMINATED ON UPPER SKIN. REPAIRED FORE FLAP IAW SRM.SDR IPXA2015061490133Skin · dentedINSPECTION TYPE: C9, A DENT WAS FOUND ON THE RT WING INBD AFT FLAP LOWER SKIN. REPAIRED IAW SRM 57-53-01-2R-1, REPAIR 1 AND SRM 51-70-10-2R-4, REPAIR 4.SDR SWAA2015062541129Support Fitting · crackedLEFT WING NR 2 FLAP TRACK SUPPORT FITTING CRACKED. REPAIRED FITTING IAW EA.SDR IPXA2015060289678Rib · crackedRIGHT INBD FLAP HAS CRACKED CLOSURE RIB ON OTBD END. 6 INCH CRACK LOCATED IN THE RADIUS OF THE UPPER TEE CAP. REPAIR IAW EO MD11-5750-57645.SDR SWAA2015061840914Flap · delaminatedLEFT WING OTBD AFT FLAP INBD TE DELAMINATED. R & R AFT FLAP IAW AMM.SDR IPXA2015053189601Skin · dentedRIGHT INBD MID FLAP HAS TWO DENTS ON LWR SURFACE 33" INBD OF OTBD EDGE 8" FWD OF T/E. REPAIRED IAW EO B747-5750-57597-A & SRM 51-70-10-2R.SDR SWAA2015060840465Skin · delaminatedRIGHT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FLAP IAW SRM.SDR AALA201506029001Wedge · delaminatedLEFT WING OTBD TE FLAP WEDGE DELAMINATED BETWEEN TRACKS 3 & 4 AT THE AFT EDGE. R & R LT WING OTBD TE FLAP WEDGE IAW EA 251646.SDR IPXA2015052989539Skin · corrodedINSPECTION TYPE: 1C, LT INBD FLAP SKIN CORRODED BETWEEN XIFH 133-141. REPAIRED CORRODED SKIN IAW EA011-5753-01-A5826, REV I/R AND EO MD11-5750-57621-A.SDR K11A201507243002Structure · corrodedLEFT OTBD MIDFLAP LOWER SIDE HAS EVIDENCE OF CORROSION AROUND NUTPLATES FOR PANEL.SDR E4EB2015120703gougedLEFT WING, OTBD FLAP UPPER SURFACE, INBD OF STATION 219, FLAP TRACK IS CHAFED & GOUGED. BLENDED OUT DAMAGED AREA, MATERIAL LOSS OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW 008-5700-38-A5864.SDR IXXA20150726099Support · corrodedNUMBER 1 FLAP SUPPORT 1, 2 & 3 BEAM HAS A HOLE WITH A DEFECT INDICATION WITH ROTARY SCAN, HOLE HAS CORROSION IN IT. HOLE REPAIRED IAW ENGINEERING DOCUMENT REA47158REA09.SDR AALA20150525006Skin · wornRIGHT OTBD FLAP, 2ND FROM OTBD WEDGE UPPER SKIN WORN. R & R SKIN ASSEMBLY IAW ESO 80096 REPAIR GENERAL 2 D 1 PAGE 601.SDR AALA20150525005Skin · wornRIGHT OTBD FLAP, 2ND FROM OTBD WEDGE LOWER SKIN WORN. R & R SKIN ASSEMBLY IAW ESO 80096 REPAIR GENERAL 2 D 1 PAGE 601.
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